US12142973B1 - Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile - Google Patents

Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile Download PDF

Info

Publication number
US12142973B1
US12142973B1 US18/495,678 US202318495678A US12142973B1 US 12142973 B1 US12142973 B1 US 12142973B1 US 202318495678 A US202318495678 A US 202318495678A US 12142973 B1 US12142973 B1 US 12142973B1
Authority
US
United States
Prior art keywords
rotor
teeth
switched reluctance
rotor teeth
stator
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
US18/495,678
Inventor
Daniel Bates
Kevin Bersch
William Gallafent
Jaroslaw Pawel Rzepecki
Alexey Kostin
Jonathan RAYNER
Markus Kaiser
Nicolas Durrande
Rupert Tombs
Ian Murphy
Xiaoyan Wang
Pierre Guern
Bhaskar Sen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Monumo Ltd
Original Assignee
Monumo Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Monumo Ltd filed Critical Monumo Ltd
Priority to US18/495,678 priority Critical patent/US12142973B1/en
Assigned to Monumo Limited reassignment Monumo Limited ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: WANG, XIAOYAN, GALLAFENT, WILLIAM, GUERN, PIERRE, KOSTIN, ALEXEY, DURRANDE, Nicolas, SEN, BHASKAR, BERSCH, KEVIN, RZEPECKI, JAROSLAW PAWEL, BATES, DANIEL, KAISER, MARKUS, MURPHY, IAN, RAYNER, JONATHAN, TOMBS, RUPERT
Priority to PCT/GB2024/052708 priority patent/WO2025088317A1/en
Application granted granted Critical
Publication of US12142973B1 publication Critical patent/US12142973B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K11/00Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
    • H02K11/30Structural association with control circuits or drive circuits
    • H02K11/33Drive circuits, e.g. power electronics
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K1/00Details of the magnetic circuit
    • H02K1/06Details of the magnetic circuit characterised by the shape, form or construction
    • H02K1/22Rotating parts of the magnetic circuit
    • H02K1/24Rotor cores with salient poles ; Variable reluctance rotors
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K1/00Details of the magnetic circuit
    • H02K1/06Details of the magnetic circuit characterised by the shape, form or construction
    • H02K1/22Rotating parts of the magnetic circuit
    • H02K1/24Rotor cores with salient poles ; Variable reluctance rotors
    • H02K1/246Variable reluctance rotors
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K19/00Synchronous motors or generators
    • H02K19/02Synchronous motors
    • H02K19/04Synchronous motors for single-phase current
    • H02K19/06Motors having windings on the stator and a variable-reluctance soft-iron rotor without windings, e.g. inductor motors
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K29/00Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices
    • H02K29/03Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices with a magnetic circuit specially adapted for avoiding torque ripples or self-starting problems
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K2213/00Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
    • H02K2213/03Machines characterised by numerical values, ranges, mathematical expressions or similar information

Definitions

  • the present disclosure relates to rotors for switched reluctance electrical motors and switched reluctance electrical motors comprising such rotors.
  • a switched reluctance motor is a type of electrical motor.
  • the stator of a SRM has windings to which switching currents are delivered to drive the motor, while the rotor has no windings or permanent magnets.
  • torque ripple i.e. a periodic increase or decrease in output torque as the rotor and motor shaft rotate.
  • Torque ripple can be particularly strong and problematic in high-torque SRMs.
  • a switched reluctance electrical motor as defined in claim 1 .
  • Embodiments of the present invention may enable switched reluctance motors that deliver high torque and exhibit low torque ripple. Embodiments may achieve this by providing rotor teeth having a transverse cross-sectional profile that is irregular but which is selected from a well-defined group of profiles.
  • FIG. 1 is a cross-sectional view of a stator and a rotor according to an embodiment
  • FIG. 2 illustrates a detail of the stator and rotor of FIG. 1 ;
  • FIG. 3 illustrates a surface profile of a slot between two teeth of the rotor of FIGS. 1 and 2 ;
  • FIG. 4 illustrates upper and lower bounds of a drive current waveform for driving stator poles of the stator of FIG. 1 ;
  • FIGS. 5 and 6 illustrate simulated performance parameters
  • FIG. 7 shows a polygon defining a range of rotor slot profiles
  • FIGS. 8 A- 10 B illustrate further example rotors.
  • a rotor of a conventional switched reluctance motor is typically provided with regularly shaped teeth, i.e. with each tooth having a flat or arcuate tip opposed to the stator and having generally straight or arcuate sidewalls.
  • SRM switched reluctance motor
  • embodiments described herein propose a rotor with rotor teeth of an irregular shape.
  • the teeth, and therefore the slots between adjacent teeth have a transverse cross-sectional profile that is irregular but which is selected from a well-defined group of profiles.
  • a particular example embodiment is described below with reference to FIGS. 1 to 4 .
  • the identified group of rotor slot profiles is then described in detail with reference to FIGS. 5 to 7 , and further example embodiments are described with reference to FIGS. 8 A to 10 B .
  • a switched reluctance motor comprising an inner rotor 1 and an outer stator 2
  • the rotor 1 is configured to be rotatable around a rotational axis of the rotor 1 (which is perpendicular to the plane of the cross-sectional view of FIG. 1 ) and to cooperate with the stator 2 , during use of the electrical motor, to provide a torque to a shaft 3 .
  • the rotor 1 may rotate counterclockwise (in the view of FIG. 1 ).
  • the electrical motor may also be operated to rotate the rotor 1 clockwise (however, in general, the “irregular” rotor teeth described in this specification are predominantly beneficial for one rotational direction, i.e. to the “counterclockwise” operation of the electrical motor in the view of FIG. 1 ).
  • the stator 2 has a generally tubular shape and comprises an inner surface 4 which, in the cross-sectional view of FIG. 1 , has a generally circular shape.
  • the stator 2 defines a plurality of circumferentially-spaced slots which extend from the inner surface 3 radially outwards to form a corresponding plurality of stator teeth 5 .
  • Respective wound field coils 6 are provided around the stator teeth 5 . These coils 6 are conductive, and are configured to provide an electromagnetic field within the motor when driven by a current. By selectively driving the coils 6 , the magnetic field within the motor may be rotated, causing the rotor 1 to be driven to rotate ( FIG.
  • stator 1 includes crosses “x” and dots “.” within the coils 6 to respectively represent electrical currents coming out or going into the respective plane at any given moment in time, when the motor is in use).
  • stator 2 may be a conventional SRM stator and the stator teeth may have a conventional, regular shape.
  • the stator 2 has an outer radius of 132.0 mm and an inner radius of 91.0 mm (i.e. the inner surface 4 of the stator 2 has a radius of 91.0 mm in the view of FIG. 1 ).
  • the rotor 1 has a substantially circular cylindrical envelope and comprises a plurality of radially extending rotor teeth 7 circumferentially-spaced apart from each other to define slots 8 between adjacent teeth.
  • the slots 8 extend co-axially along an otherwise circular cylindrical rotor 1 .
  • FIG. 2 is a close-up of a portion 9 of the SRM of FIG. 1 , showing one of the rotor teeth 7 in more detail (each rotor tooth 7 has generally the same shape). In the cross-sectional view of FIG.
  • the teeth 7 have a generally smooth, curved radially outer surface and “irregularly” shaped sidewalls 11 , 12 .
  • the sidewalls 11 , 12 of any given tooth are asymmetric, i.e. the “sidewalls” 11 , 12 are not mirror images of each other (e.g. unlike the rightmost sidewall 12 , the leftmost sidewall 11 comprises an overhanging portion 13 ).
  • the rotor 1 and the stator 2 are dimensioned so that a small air gap is provided between the rotor teeth 7 and the stator 2 . In the embodiment of FIG. 1 , the air gap is 1 mm.
  • the surface profile 14 of the slots 8 may be expressed conveniently using a polar coordinate system centred on the rotational axis of the rotor 1 , that is using polar coordinates comprising a radial coordinate defining a distance from the centre of the rotational axis and an angular coordinate defining an angle from a reference direction. Further, the rotor slot surface profile 14 may be expressed in normalised radial and angular coordinates.
  • the “normalised radial coordinate r norm ” may be defined by
  • r 0 is the distance from the rotational axis
  • r min is minimum radius of the rotor 1 (i.e. the shortest distance from the rotational axis to the surface profile 14 of the rotor slot 8 )
  • r max is the rotor's outer diameter, as illustrated in FIG. 1 .
  • the normalised radial coordinate may take values in the interval 0 ⁇ r norm ⁇ 1 (since r min ⁇ r norm ⁇ r max ).
  • ⁇ n ⁇ o ⁇ r ⁇ m ⁇ 0 - ⁇ m ⁇ i ⁇ n ⁇ m ⁇ ax - ⁇ m ⁇ i ⁇ n
  • ⁇ 0 is the angle from a reference direction (by convention ⁇ 0 may increase in counter-clockwise direction)
  • ⁇ min and ⁇ max are angles indicating the end points of one example slot 8 in clockwise direction (as illustrated in FIG. 1 ).
  • ⁇ norm is independent of the choice of the reference direction.
  • the value of the normalised angular coordinate ⁇ norm is not restricted to the interval between 0 and 1.
  • the line 15 in the graph of FIG. 3 represent the surface profile 14 of opposed sidewalls of a pair of adjacent rotor teeth 7 and which together define a slot 8 , expressed in the above described normalised radial and angular coordinates.
  • Other embodiments may comprise rotor slots having the profile 15 but having different values for the parameters r min , r max , ⁇ max , and ⁇ max (corresponding example embodiments are described below with reference to FIGS. 8 A to 10 B ).
  • the profile 15 can be expressed as a piecewise-linear function defined by a sequence of coordinates (i.e. each coordinate is an ordered pair comprising a normalised angular value and a normalised radial value).
  • the profile 15 can readily be reconstructed from the sequence by linear interpolation between successive coordinates.
  • the “Well-known text (WKT) representation” is a commonly employed representation that uses such sequences of coordinates to represent vector geometry objects (e.g. lines, polygons and other geometrical objects).
  • WKT format is included in the ISO-IEC 13249-3:2016 standard.
  • the WKT representation of the profile 15 in ( ⁇ norm , r norm ) coordinates, reads:
  • the coils 6 may be driven by temporally varying electrical currents (synchronised with the rotational position of the rotor 1 ).
  • the SRM motor May comprise an inverter unit (not shown in FIG. 1 ) configured to provide the corresponding drive currents. Any known and suitable inverter unit may be used.
  • the drive currents are periodic and may be defined by specifying a waveform (i.e. a temporal profile of current values over one cycle). More specifically, the SRM of FIG. 1 can be operated as a 3-phase SRM. In this case, the coils 6 may be driven with respectively phase-shifted current waveforms (coils with the same reference numeral 6 k , where K ⁇ A,B,C ⁇ , in FIG.
  • coils 6 A, 6 B and 6 c are driven by a corresponding current I K ( ⁇ ) (where ⁇ is a rotation angle of the rotor 1 ) which satisfies
  • the drive currents for the SRM of FIG. 1 may be defined by a single-valued function specifying current values over one period
  • a suitable waveform for driving the motor of FIG. 1 may be readily identified by performing an appropriate computational simulation of the motor during operation (conventional and commercially available simulation software may be used to perform such simulations). For example, such simulations may be used to iteratively improve/optimise an initial waveform “guess” (the simulation may take limitations of the inverter into account, for example, the inverter output may be limited to positive voltages/currents). In this way, example current waveforms for driving the motor of FIG. 1 have been identified by the inventors and are now described with reference to FIG. 4 . The waveforms 41 and 43 shown in the graph of FIG.
  • the SRM of FIG. 1 may be operated with a drive current waveform which lies in between the upper and lower bounds 41 , 43 , i.e. P lower (t) ⁇ I K (t) ⁇ P upper (t).
  • the upper and lower bounds 41 , 43 may be defined using a sequence of piecewise polynomial functions. More specifically, the upper and lower bounds 41 , 43 may be expressed as piecewise cubic polynomials on an evenly spaced grid.
  • piecewise cubic functions P(t; ⁇ x i ⁇ , ⁇ c ji ⁇ ) may be defined by breakpoints ⁇ x i ⁇ , coefficients ⁇ c ji ⁇ , and the following construction:
  • FIG. 5 illustrates the results for a set of simulated tooth shapes, each point in the plot showing a result for a given tooth shape.
  • FIG. 5 illustrates the results of approximately one million different tooth shapes (the outer diameter r max of the rotor and the number of rotor teeth n r is same for all shown data points).
  • the circle 51 in FIG. 5 indicates a conventional design with regularly shaped rotor teeth which results in a predicted output torque of less than 205 N/m with a torque ripple of more than 14%.
  • FIG. 6 shows a group of data points 53 of extracted from FIG. 5 which are identified as a group of optimal tooth shapes, specifically shapes resulting in a predicted output torque exceeding 227 N/m and torque ripple of less than 2% (when driven with a drive current waveform that lies within the upper and lower bounds 41 , 43 described above).
  • the circle 55 indicates the predicted performance for the tooth shape shown in FIGS. 1 to 3 which results in a predicted torque exceeding 228 N/m and torque ripple of less than 0.5%.
  • the identified group of tooth shapes correspond to a set of slot profiles that, when expressed in normalised radial and angular coordinates, are contained within a region 57 enclosed by a polygon 59 as shown in FIG. 7 .
  • the polygon 20 defines boundaries of the enclosed region 57 in the (normalised) polar coordinate system and embodiments lie within the region 57 .
  • the polygon 59 can be defined by a sequence of normalised coordinates which represent the polygon's vertices (each coordinate is an ordered pair comprising a normalised angular value and a normalised radial value.
  • the polygon 59 can then be readily reconstructed from the sequence by linear interpolation between vertices (i.e. by connecting successive coordinates with a straight line).
  • the WKT representation of the polygon 59 in ( ⁇ norm , r norm ) coordinates, reads:
  • Conventional and readily available software tools may be used to plot the polygon 59 or the profile 15 (e.g. online WKT plotting tools such as on https://www.geometrymapper.com) or to test whether a particular surface profile (expressed in ( ⁇ norm , r norm ) coordinates) lies within the area enclosed by the polygon 59 .
  • the C/C++ library “GEOS” may be used to read in i) a WKT representation of the surface profile in question and ii) the above WKT representation of the polygon 59 , and to implement the test “GEOSContains” to determine whether the profile in question lies (completely) within the polygonal area 57 .
  • the points 53 show predicted torque and toque ripple values for more than 10,000 different rotor slot profiles selected from the group of profiles defined by polygon 59 . It is evident that each of these rotor slot profiles has improved predicted torque and torque ripple values (specifically output torque exceeding 227 N/m and torque ripple of less than 2% for the above described operating conditions) compared to the aforementioned conventional design.
  • the number of rotor teeth and stator poles may be different than the corresponding numbers in the embodiment of FIG. 1 (i.e. the rotor may have more than or less than 12 rotor teeth and the stator may have more than or less than 16 stator poles).
  • Nr rotor teeth
  • Ns stator poles
  • FIGS. 8 A to 10 B illustrate variations of the above described rotor 1 .
  • FIG. 8 A is cross-sectional view of rotor 61 comprising four rotor teeth. The slots between adjacent teeth of the rotor 61 have the transverse cross-sectional profile 15 of FIG. 4 (i.e. a profile that lies within the polygon 59 ).
  • FIG. 8 B is a table containing numerical values of parameters specifying the rotor 61 such as the minimum radius Imin, the outer diameter r max , the angles ⁇ min and ⁇ max indicating the end points of a slot, and the shaft diameter.
  • FIGS. 8 A is cross-sectional view of rotor 61 comprising four rotor teeth.
  • the slots between adjacent teeth of the rotor 61 have the transverse cross-sectional profile 15 of FIG. 4 (i.e. a profile that lies within the polygon 59 ).
  • FIG. 8 B is a table containing numerical values of parameters specifying the rotor 61 such as the
  • FIGS. 9 A and 10 A are cross-sectional views of rotors 63 , 65 respectively comprising 31 and 48 rotor teeth (the slots between adjacent teeth of the rotors 63 , 65 have the transverse cross-sectional profile 15 of FIG. 4 ).
  • the tables of FIGS. 9 B and 10 B respectively contain numerical values of parameters specifying the rotors 63 , 65 .
  • the rotors 61 , 63 , 65 of FIGS. 8 A, 9 A and 10 A are intended to be used with appropriately configured stators (e.g. conventional stators that are appropriately dimensioned and that have a suitable number of stator poles).
  • a corresponding stator for use with rotor 61 , 63 or 65 may have respectively 6, 48 or 72 stator poles.
  • the substantially circular cylindrical envelope of the above described rotors may have a diameter in a range of 20 mm to 250 mm (preferably in a range 100 mm to 150 mm).
  • the length of the above described rotors may be in the range of 20 mm to 250 mm (i.e. the rotors may extend along their rotational axis for a length in the range of 20 mm to 250 mm). In some embodiments, the rotor length may be in the range of 100 mm to 150 mm.
  • the above described embodiments may be manufactured with known manufacturing methods (e.g. die casting, machining, additive manufacturing, and the like). It is to be understood that, as in conventional SRMs, in the above described embodiments the rotors, e.g. rotor 1 , may not comprise permanent magnets or windings but may comprise a ferroelectric material (e.g. iron).
  • a ferroelectric material e.g. iron

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Abstract

A switched reluctance electrical motor comprises a rotor having a substantially circular cylindrical envelope with a diameter in a range of 50 mm to 300 mm and a length in the range of 20 mm to 250 mm. The rotor comprises a plurality of radially extending rotor teeth. A switched reluctance electrical motor further comprises a stator surrounding the rotor and comprising a plurality of stator poles. The rotor teeth are circumferentially-spaced apart from each other to define slots between adjacent teeth that, expressed in normalised angular and radial coordinates, have a cross-sectional profile transverse to an axis of rotation of the rotor, lying within a well-defined polygonal region.

Description

TECHNICAL FIELD
The present disclosure relates to rotors for switched reluctance electrical motors and switched reluctance electrical motors comprising such rotors.
BACKGROUND
A switched reluctance motor (SRM) is a type of electrical motor. The stator of a SRM has windings to which switching currents are delivered to drive the motor, while the rotor has no windings or permanent magnets. It is known that conventional SRM designs suffer from torque ripple, i.e. a periodic increase or decrease in output torque as the rotor and motor shaft rotate. Torque ripple can be particularly strong and problematic in high-torque SRMs. Thus, there is a need to provide improved SRMs that deliver high torque and exhibit low torque ripple.
SUMMARY
According to a first aspect of the invention, there is provided a switched reluctance electrical motor as defined in claim 1.
Embodiments of the present invention may enable switched reluctance motors that deliver high torque and exhibit low torque ripple. Embodiments may achieve this by providing rotor teeth having a transverse cross-sectional profile that is irregular but which is selected from a well-defined group of profiles.
According to a second aspect of the invention, there is provided a system as defined in claim 8.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a cross-sectional view of a stator and a rotor according to an embodiment;
FIG. 2 illustrates a detail of the stator and rotor of FIG. 1 ;
FIG. 3 illustrates a surface profile of a slot between two teeth of the rotor of FIGS. 1 and 2 ;
FIG. 4 illustrates upper and lower bounds of a drive current waveform for driving stator poles of the stator of FIG. 1 ;
FIGS. 5 and 6 illustrate simulated performance parameters;
FIG. 7 shows a polygon defining a range of rotor slot profiles; and
FIGS. 8A-10B illustrate further example rotors.
DETAILED DESCRIPTION
A rotor of a conventional switched reluctance motor (SRM) is typically provided with regularly shaped teeth, i.e. with each tooth having a flat or arcuate tip opposed to the stator and having generally straight or arcuate sidewalls. To enable electrical motors that deliver high torque and exhibit low torque ripple, embodiments described herein propose a rotor with rotor teeth of an irregular shape. In other words, the teeth, and therefore the slots between adjacent teeth, have a transverse cross-sectional profile that is irregular but which is selected from a well-defined group of profiles. A particular example embodiment is described below with reference to FIGS. 1 to 4 . The identified group of rotor slot profiles is then described in detail with reference to FIGS. 5 to 7 , and further example embodiments are described with reference to FIGS. 8A to 10B.
With reference to FIG. 1 , a switched reluctance motor comprising an inner rotor 1 and an outer stator 2 will now be described. The rotor 1 is configured to be rotatable around a rotational axis of the rotor 1 (which is perpendicular to the plane of the cross-sectional view of FIG. 1 ) and to cooperate with the stator 2, during use of the electrical motor, to provide a torque to a shaft 3. In particular, during use of the electrical motor, the rotor 1 may rotate counterclockwise (in the view of FIG. 1 ). It is to be understood that the electrical motor may also be operated to rotate the rotor 1 clockwise (however, in general, the “irregular” rotor teeth described in this specification are predominantly beneficial for one rotational direction, i.e. to the “counterclockwise” operation of the electrical motor in the view of FIG. 1 ).
The stator 2 has a generally tubular shape and comprises an inner surface 4 which, in the cross-sectional view of FIG. 1 , has a generally circular shape. The stator 2 defines a plurality of circumferentially-spaced slots which extend from the inner surface 3 radially outwards to form a corresponding plurality of stator teeth 5. Respective wound field coils 6 are provided around the stator teeth 5. These coils 6 are conductive, and are configured to provide an electromagnetic field within the motor when driven by a current. By selectively driving the coils 6, the magnetic field within the motor may be rotated, causing the rotor 1 to be driven to rotate (FIG. 1 includes crosses “x” and dots “.” within the coils 6 to respectively represent electrical currents coming out or going into the respective plane at any given moment in time, when the motor is in use). It is to be understood that the stator 2 may be a conventional SRM stator and the stator teeth may have a conventional, regular shape. In the embodiment of FIG. 1 , the stator 2 has an outer radius of 132.0 mm and an inner radius of 91.0 mm (i.e. the inner surface 4 of the stator 2 has a radius of 91.0 mm in the view of FIG. 1 ).
The rotor 1 has a substantially circular cylindrical envelope and comprises a plurality of radially extending rotor teeth 7 circumferentially-spaced apart from each other to define slots 8 between adjacent teeth. The slots 8 extend co-axially along an otherwise circular cylindrical rotor 1. This means that the teeth 7 (and correspondingly the slots 8) have the same cross-sectional profile along the entire length of the rotor 1 (rotor skew can be implemented as required). FIG. 2 is a close-up of a portion 9 of the SRM of FIG. 1 , showing one of the rotor teeth 7 in more detail (each rotor tooth 7 has generally the same shape). In the cross-sectional view of FIG. 2 , the teeth 7 have a generally smooth, curved radially outer surface and “irregularly” shaped sidewalls 11,12. In the illustrated example, the sidewalls 11,12 of any given tooth are asymmetric, i.e. the “sidewalls” 11, 12 are not mirror images of each other (e.g. unlike the rightmost sidewall 12, the leftmost sidewall 11 comprises an overhanging portion 13). The rotor 1 and the stator 2 are dimensioned so that a small air gap is provided between the rotor teeth 7 and the stator 2. In the embodiment of FIG. 1 , the air gap is 1 mm.
As the cross-section of the rotor 1 generally exhibits a nr-fold rotation symmetry (where nr is the number of rotor teeth 7 or slots 8, i.e. nr=12 in the embodiment of FIG. 1 ) around the rotational axis of the rotor 1, the surface profile 14 of the slots 8 may be expressed conveniently using a polar coordinate system centred on the rotational axis of the rotor 1, that is using polar coordinates comprising a radial coordinate defining a distance from the centre of the rotational axis and an angular coordinate defining an angle from a reference direction. Further, the rotor slot surface profile 14 may be expressed in normalised radial and angular coordinates.
In particular, the “normalised radial coordinate rnorm” may be defined by
r n o r m = r 0 - r m i n r m ax - r m i n ,
where r0 is the distance from the rotational axis, rmin is minimum radius of the rotor 1 (i.e. the shortest distance from the rotational axis to the surface profile 14 of the rotor slot 8), and rmax is the rotor's outer diameter, as illustrated in FIG. 1 . The normalised radial coordinate may take values in the interval 0≤rnorm≤1 (since rmin≤rnorm≤rmax). For the particular embodiment of FIGS. 1 and 2 , the values for minimum and maximum radius are rmin=66.8 mm and rmax=90.0 mm (the diameter of the shaft 3 of FIG. 1 is 25 mm).
Similarly, the “normalised angular coordinate φnorm” may be defined by
φ n o r m = φ 0 - φ m i n φ m ax - φ m i n
where φ0 is the angle from a reference direction (by convention φ0 may increase in counter-clockwise direction), φmin and φmax are angles indicating the end points of one example slot 8 in clockwise direction (as illustrated in FIG. 1 ). It is to be understood that φnorm is independent of the choice of the reference direction. Unlike the normalised radial coordinate rnorm, the value of the normalised angular coordinate φnorm is not restricted to the interval between 0 and 1. For the particular embodiment of FIGS. 1 and 2 , the values for φmin and φmax are φmin=6.0 deg and φmin=24.0 deg.
The line 15 in the graph of FIG. 3 represent the surface profile 14 of opposed sidewalls of a pair of adjacent rotor teeth 7 and which together define a slot 8, expressed in the above described normalised radial and angular coordinates. Other embodiments may comprise rotor slots having the profile 15 but having different values for the parameters rmin, rmax, φmax, and φmax (corresponding example embodiments are described below with reference to FIGS. 8A to 10B).
The profile 15 can be expressed as a piecewise-linear function defined by a sequence of coordinates (i.e. each coordinate is an ordered pair comprising a normalised angular value and a normalised radial value). The profile 15 can readily be reconstructed from the sequence by linear interpolation between successive coordinates. The “Well-known text (WKT) representation” is a commonly employed representation that uses such sequences of coordinates to represent vector geometry objects (e.g. lines, polygons and other geometrical objects). A definition of the WKT format is included in the ISO-IEC 13249-3:2016 standard. The WKT representation of the profile 15, in (φnorm, rnorm) coordinates, reads:
    • LINESTRING (0 1, 0.00373 0.97444, −0.01024 0.94839, −0.0265 0.92328, −0.03943 0.89703, −0.04526 0.86906, −0.04594 0.84067, −0.04295 0.81238, −0.03731 0.78436, −0.02967 0.75667, −0.02048 0.72929, −0.01004 0.70223, 0.00141 0.67544, 0.0137 0.64889, 0.02612 0.6224, 0.03835 0.59585, 0.05034 0.56922, 0.06206 0.54252, 0.07345 0.51572, 0.08445 0.4888, 0.09494 0.46175, 0.10476 0.43453, 0.11364 0.40709, 0.12106 0.37937, 0.12719 0.35143, 0.13293 0.32342, 0.13828 0.29537, 0.14324 0.26726, 0.14781 0.23911, 0.15199 0.21092, 0.18115 0.18429, 0.21094 0.15813, 0.24146 0.13256, 0.27285 0.10771, 0.30526 0.08379, 0.33896 0.06109, 0.37422 0.0401, 0.41151 0.02164, 0.45133 0.00728, 0.49386 0.00013, 0.53699 0.00382, 0.57613 0.01912, 0.6066 0.04458, 0.62793 0.07579, 0.64228 0.10965, 0.6517 0.14468, 0.68136 0.16329, 0.70986 0.18309, 0.73562 0.20527, 0.74613 0.2338, 0.75517 0.26362, 0.76738 0.29267, 0.78068 0.32139, 0.7946 0.34991, 0.80891 0.37829, 0.82352 0.40657, 0.83777 0.43497, 0.85102 0.4637, 0.8633 0.49273, 0.87467 0.522, 0.88515 0.5515, 0.8948 0.58119, 0.90366 0.61105, 0.91176 0.64105, 0.91914 0.67118, 0.92583 0.70142, 0.93188 0.73176, 0.9373 0.76217, 0.94216 0.79266, 0.9471 0.82313, 0.95237 0.85357, 0.9581 0.88394, 0.96448 0.91424, 0.97187 0.94438, 0.98125 0.97415, 1 1).
To generate torque, the coils 6 may be driven by temporally varying electrical currents (synchronised with the rotational position of the rotor 1). To this end, the SRM motor May comprise an inverter unit (not shown in FIG. 1 ) configured to provide the corresponding drive currents. Any known and suitable inverter unit may be used. In general, the drive currents are periodic and may be defined by specifying a waveform (i.e. a temporal profile of current values over one cycle). More specifically, the SRM of FIG. 1 can be operated as a 3-phase SRM. In this case, the coils 6 may be driven with respectively phase-shifted current waveforms (coils with the same reference numeral 6 k, where K∈{A,B,C}, in FIG. 1 are driven with the same phase-shifted waveform), i.e. coils 6A, 6B and 6 c are driven by a corresponding current IK(θ) (where θ is a rotation angle of the rotor 1) which satisfies
I A ( θ ) = I C ( θ - 2 π 3 ) = I B ( θ - 4 π 3 ) .
The current waveform is continuous and periodic, i.e. IK(θ)=IK(θ+2π) for all angles θ. Further, the nr=12-fold symmetry of the rotor 1 means that the current waveform repeats itself 12-fold over one revolution of the rotor 1, i.e. the period of the current waveform is given by
T = 1 f * n r
(where f is the frequency of rotation of the rotor 1), and the rotational angle of rotor 1 at time t is therefore
θ ( t ) = 2 π t T .
Thus, the drive currents for the SRM of FIG. 1 may be defined by a single-valued function specifying current values over one period
T = 1 f * n r .
A suitable waveform for driving the motor of FIG. 1 may be readily identified by performing an appropriate computational simulation of the motor during operation (conventional and commercially available simulation software may be used to perform such simulations). For example, such simulations may be used to iteratively improve/optimise an initial waveform “guess” (the simulation may take limitations of the inverter into account, for example, the inverter output may be limited to positive voltages/currents). In this way, example current waveforms for driving the motor of FIG. 1 have been identified by the inventors and are now described with reference to FIG. 4 . The waveforms 41 and 43 shown in the graph of FIG. 4 represent respectively an upper waveform bound Pupper (t) and a lower waveform bound Plower (t) which specify normalised current values over one period T (i.e. the current values are normalised with respect to a nominal drive current value which may represent a drive current at full drive power, e.g. 200 A). The SRM of FIG. 1 may be operated with a drive current waveform which lies in between the upper and lower bounds 41, 43, i.e. Plower(t)<IK(t)<Pupper(t).
The upper and lower bounds 41, 43 may be defined using a sequence of piecewise polynomial functions. More specifically, the upper and lower bounds 41, 43 may be expressed as piecewise cubic polynomials on an evenly spaced grid. Mathematically, piecewise cubic functions P(t;{xi},{cji}) may be defined by breakpoints {xi}, coefficients {cji}, and the following construction:
k ( x ) = max { i : x i x , i = 0 , 1 , 2 , } P ( t ; { x i } , { c j i } ) = m = 0 3 c m k ( x ) ( t - x k ( t ) ) 3 - m
The respective break points breakpoints {xi} and coefficients {cji} for the upper bound and lower bounds 41, 43 of FIG. 4 are given respectively in Table 1 and Table 2.
TABLE 1
x[i] c[0, i] c[1, i] c[2, i] c[3, i]
0 −373.323 33.58275 −2.32853 0.34205
0.03125 173.0888 −1.41625 −1.32332 0.29068
0.0625 −375.739 14.81082 −0.90474 0.25323
0.09375 349.2132 −20.4147 −1.07986 0.22795
0.125 −247.251 12.32403 −1.3327 0.18493
0.15625 199.1973 −10.8558 −1.28681 0.14777
0.1875 −131.193 7.81896 −1.38172 0.10304
0.21875 157.7718 −4.48036 −1.27738 0.06349
0.25 59.36887 10.31074 −1.09518 0.02401
0.28125 −232.297 15.87657 −0.27683 0.00167
0.3125 107.0701 −5.9013 0.0349 0.00143
0.34375 −90.1919 4.13652 −0.02025 3.00E−05
0.375 215.3981 −4.31896 −0.02595 0.00068
0.40625 639.1797 15.87461 0.33516 0.00222
0.4375 −857.131 75.7977 3.19992 0.04771
0.46875 125.082 −4.55828 5.42615 0.19557
0.5 −284.438 7.16815 5.50771 0.3645
0.53125 46.35379 −19.4979 5.12241 0.53494
0.5625 147.8982 −15.1522 4.03959 0.67739
0.59375 −228.133 −1.28676 3.52587 0.79334
0.625 321.0824 −22.6742 2.77709 0.8953
0.65625 −620.243 7.42726 2.30062 0.96974
0.6875 657.6039 −50.7205 0.94771 1.02996
0.71875 −182.019 10.92985 −0.29575 1.03012
0.75 270.2227 −6.13444 −0.14589 1.02599
0.78125 −227.367 19.19894 0.26237 1.02369
0.8125 −276.057 −2.11675 0.79619 1.0437
0.84375 −449.991 −27.9971 −0.14486 1.05809
0.875 319.3301 −70.1837 −3.21301 1.01249
0.90625 786.4246 −40.2465 −6.66396 0.85329
0.9375 61.19588 33.48082 −6.87538 0.62974
0.96875 −60.1086 39.21793 −4.60355 0.44944
TABLE 2
x[i] c[0, i] c[1, i] c[2, i] c[3, i]
0 −305.845 28.92415 −2.20194 0.32877
0.03125 130.2671 0.25122 −1.29021 0.27888
0.0625 −325.198 12.46376 −0.89287 0.24278
0.09375 287.1394 −18.0235 −1.06661 0.21712
0.125 −186.666 8.8958 −1.35185 0.17495
0.15625 50.51431 −8.60416 −1.34274 0.1357
0.1875 170.1673 −3.86844 −1.73251 0.08688
0.21875 85.98653 12.08474 −1.47575 0.03415
0.25 −251.979 20.14597 −0.46854 0.00246
0.28125 55.369 −3.47709 0.05236 −0.0002
0.3125 −46.396 1.71375 −0.00274 −0.00027
0.34375 85.52181 −2.63587 −0.03156 −0.0001
0.375 −276.477 5.3818 0.05425 −0.00105
0.40625 1480.673 −20.5379 −0.41937 −0.00253
0.4375 −1448.62 118.2752 2.63492 0.00949
0.46875 232.5341 −17.5331 5.78311 0.16313
0.5 −164.674 4.26695 5.36854 0.33382
0.53125 −96.2515 −11.1712 5.15278 0.50073
0.5625 205.3256 −20.1948 4.17259 0.64791
0.59375 −218.226 −0.94552 3.51196 0.76485
0.625 289.0866 −21.4042 2.81353 0.86701
0.65625 −567.38 5.69763 2.3227 0.94286
0.6875 579.6662 −47.4942 1.01655 1.00369
0.71875 −121.858 6.84946 −0.2536 1.00677
0.75 189.2459 −4.57477 −0.18251 1.00181
0.78125 −129.29 13.16704 0.086 0.99742
0.8125 −244.443 1.04608 0.53016 1.00902
0.84375 −511.494 −21.8705 −0.12061 1.01914
0.875 272.9554 −69.823 −2.98603 0.97841
0.90625 868.1212 −44.2335 −6.55029 0.82524
0.9375 31.17326 37.15289 −6.77156 0.60384
0.96875 −118.947 40.07539 −4.35818 0.42946
Further, by simulating the operation of the switched reluctance motors, the inventors have found that the output of such motors can be improved over designs employing conventional regularly shaped rotor teeth, with the use of irregularly shaped teeth such as those illustrated in FIGS. 1 to 3 . FIG. 5 illustrates the results for a set of simulated tooth shapes, each point in the plot showing a result for a given tooth shape. In particular, FIG. 5 illustrates the results of approximately one million different tooth shapes (the outer diameter rmax of the rotor and the number of rotor teeth nr is same for all shown data points). The large number of simulations performed and illustrated means that the data points in the Figure are not necessarily individually identifiable and the data set is shown more as shading where darker areas indicate a greater density of data points and lighter areas indicate a lower density of data points. More specifically, the simulation results shown in FIGS. 5 and 6 correspond to a predicted performance of the motor at an operating point of f=2768 rotations per minute and a nominal drive current of Inorm=200 A.
The circle 51 in FIG. 5 indicates a conventional design with regularly shaped rotor teeth which results in a predicted output torque of less than 205 N/m with a torque ripple of more than 14%. FIG. 6 shows a group of data points 53 of extracted from FIG. 5 which are identified as a group of optimal tooth shapes, specifically shapes resulting in a predicted output torque exceeding 227 N/m and torque ripple of less than 2% (when driven with a drive current waveform that lies within the upper and lower bounds 41, 43 described above). In particular, the circle 55 indicates the predicted performance for the tooth shape shown in FIGS. 1 to 3 which results in a predicted torque exceeding 228 N/m and torque ripple of less than 0.5%.
The identified group of tooth shapes correspond to a set of slot profiles that, when expressed in normalised radial and angular coordinates, are contained within a region 57 enclosed by a polygon 59 as shown in FIG. 7 . Thus, the polygon 20 defines boundaries of the enclosed region 57 in the (normalised) polar coordinate system and embodiments lie within the region 57. In other words, all slot profiles that lie within the polygon 59 of FIG. 7 exhibit desired torque and torque ripple characteristics, e.g. a predicted output torque exceeding 227 N/m and torque ripple of less than 2% (for f=2768 rotations per minute and Inorm=200 A). The polygon 59 can be defined by a sequence of normalised coordinates which represent the polygon's vertices (each coordinate is an ordered pair comprising a normalised angular value and a normalised radial value. The polygon 59 can then be readily reconstructed from the sequence by linear interpolation between vertices (i.e. by connecting successive coordinates with a straight line). The WKT representation of the polygon 59, in (φnorm, rnorm) coordinates, reads:
    • POLYGON ((0.42242−0.00244, 0.41315 0.00244, 0.37738 0.01113, 0.31221 0.06593, 0.27282 0.09056, 0.21648 0.12963, 0.11751 0.20699, 0.11737 0.24054, 0.11385 0.28571, 0.09277 0.34885, 0.07981 0.4127, 0.02934 0.55067, −0.02808 0.69306, −0.0469 0.75422, −0.05749 0.80562, −0.05986 0.84371, −0.05629 0.87459, −0.04921 0.90035, −0.03859 0.92121, −0.00235 0.97436, −0.00338 1.00302, 0.00461 1.00413, 0.00934 0.974, −0.00366 0.94692, −0.02113 0.92063, −0.03404 0.89499, −0.03991 0.87057, −0.03991 0.83394, −0.03286 0.79365, −0.0223 0.75824, −0.00587 0.71551, 0.00822 0.68376, 0.06916 0.56091, 0.09615 0.49741, 0.11259 0.45224, 0.12671 0.40451, 0.13498 0.3602, 0.14082 0.33968, 0.14904 0.29816, 0.15258 0.26618, 0.1608 0.24664, 0.17371 0.22222, 0.21009 0.18559, 0.4108 0.08059, 0.48005 0.0464, 0.60211 0.12088, 0.65747 0.20825, 0.67606 0.23077, 0.70775 0.28083, 0.7208 0.31071, 0.73963 0.34012, 0.77844 0.39027, 0.80047 0.41514, 0.83099 0.47009, 0.86385 0.53724, 0.89319 0.61661, 0.91432 0.70208, 0.94603 0.86837, 0.96484 0.94541, 0.97672 0.97992, 0.99448 1.00208, 0.9972 1.00479, 1.00055 1.00474, 1.0045 1.0019, 1.00464 0.99842, 1.00117 0.99512, 0.98592 0.96825, 0.98005 0.94139, 0.973 0.88034, 0.9683 0.78621, 0.96361 0.73126, 0.9542 0.67131, 0.94131 0.61905, 0.94012 0.60538, 0.93073 0.5602, 0.91667 0.50916, 0.91075 0.48072, 0.89076 0.41467, 0.86963 0.35973, 0.85197 0.32177, 0.83451 0.2906, 0.82746 0.26984, 0.81455 0.07204, 0.81559 0.0617, 0.81103 0.05861, 0.80013 0.04309, 0.79612 0.04157, 0.67276 0.01345, 0.61279 0.00367, 0.57054−0.00122, 0.55634−0.00122, 0.54941−0.00366, 0.48122−0.00366, 0.42242 −0.00244)).
Conventional and readily available software tools may be used to plot the polygon 59 or the profile 15 (e.g. online WKT plotting tools such as on https://www.geometrymapper.com) or to test whether a particular surface profile (expressed in (φnorm, rnorm) coordinates) lies within the area enclosed by the polygon 59. For example, the C/C++ library “GEOS” may be used to read in i) a WKT representation of the surface profile in question and ii) the above WKT representation of the polygon 59, and to implement the test “GEOSContains” to determine whether the profile in question lies (completely) within the polygonal area 57.
Referring back to the graph of FIG. 6 , the points 53 show predicted torque and toque ripple values for more than 10,000 different rotor slot profiles selected from the group of profiles defined by polygon 59. It is evident that each of these rotor slot profiles has improved predicted torque and torque ripple values (specifically output torque exceeding 227 N/m and torque ripple of less than 2% for the above described operating conditions) compared to the aforementioned conventional design.
Various modifications will be apparent to those skilled in the art. For example, in some embodiments, the number of rotor teeth and stator poles may be different than the corresponding numbers in the embodiment of FIG. 1 (i.e. the rotor may have more than or less than 12 rotor teeth and the stator may have more than or less than 16 stator poles).
By way of example only, the following provides indicative numbers of slots and poles for different SRM designs:
    • three-phase SRMs: 6/2; 6/4; 6/8; 6/14; 12/8; 18/12; 24/16;
    • four-phase SRMs: 8/6; 8/10; 16/12; 24/18; 32/24;
    • five-phase SRMs: 10/4; 10/6; 10/8; 10/12;
    • xix-phase SRMs: 12/10; 12/14; 24/20;
    • seven-phase SRMs: 14/10; 14/12; 14/16.
It is noted in particular that it may be advantageous to have a number of rotor teeth (poles) Nr that is greater than the number of stator poles Ns. Such designs may have relatively high efficiency, output power and lower torque ripple. For example, Nr=2*Ns−2, so 10/6, 14/8, and 18/10 etc.
FIGS. 8A to 10B illustrate variations of the above described rotor 1. FIG. 8A is cross-sectional view of rotor 61 comprising four rotor teeth. The slots between adjacent teeth of the rotor 61 have the transverse cross-sectional profile 15 of FIG. 4 (i.e. a profile that lies within the polygon 59). FIG. 8B is a table containing numerical values of parameters specifying the rotor 61 such as the minimum radius Imin, the outer diameter rmax, the angles φmin and φmax indicating the end points of a slot, and the shaft diameter. Similarly, FIGS. 9A and 10A are cross-sectional views of rotors 63, 65 respectively comprising 31 and 48 rotor teeth (the slots between adjacent teeth of the rotors 63, 65 have the transverse cross-sectional profile 15 of FIG. 4 ). The tables of FIGS. 9B and 10B respectively contain numerical values of parameters specifying the rotors 63, 65. It is to be understood that the rotors 61, 63, 65 of FIGS. 8A, 9A and 10A are intended to be used with appropriately configured stators (e.g. conventional stators that are appropriately dimensioned and that have a suitable number of stator poles). For example, a corresponding stator for use with rotor 61, 63 or 65 may have respectively 6, 48 or 72 stator poles.
In embodiments, the substantially circular cylindrical envelope of the above described rotors may have a diameter in a range of 20 mm to 250 mm (preferably in a range 100 mm to 150 mm).
In embodiments, the length of the above described rotors may be in the range of 20 mm to 250 mm (i.e. the rotors may extend along their rotational axis for a length in the range of 20 mm to 250 mm). In some embodiments, the rotor length may be in the range of 100 mm to 150 mm.
The above described embodiments may be manufactured with known manufacturing methods (e.g. die casting, machining, additive manufacturing, and the like). It is to be understood that, as in conventional SRMs, in the above described embodiments the rotors, e.g. rotor 1, may not comprise permanent magnets or windings but may comprise a ferroelectric material (e.g. iron).

Claims (7)

The invention claimed is:
1. A switched reluctance electrical motor comprising:
a rotor having a substantially circular cylindrical envelope with a diameter in a range of 50 mm to 300 mm and a length in the range of 20 mm to 250 mm, and comprising a plurality of radially extending rotor teeth, each of the rotor teeth having a smooth, curved radially outer surface and asymmetric side walls, one side wall of the asymmetric side walls having an overhanging portion that projects from each of the rotor teeth in a rotational direction, and
a stator surrounding the rotor and comprising a plurality of stator poles, and the rotor teeth are circumferentially-spaced apart from each other to define slots between adjacent teeth formed by the asymmetric side walls of adjacent rotor teeth that, expressed in normalised angular and radial coordinates φnorm and rnorm respectively defined by
φ n o r m = φ 0 - φ m i n φ m ax - φ m i n and r n o r m = r 0 - r m i n r m ax - r m i n ,
rnorm being less than or equal to 1 and greater than or equal to 0, have a cross-sectional profile transverse to an axis of rotation of the rotor, lying within a polygonal region having a corresponding Well-known text, WKT, representation of:
POLYGON ((0.42242 −0.00244, 0.41315 0.00244, 0.37738 0.01113, 0.31221 0.06593, 0.27282 0.09056, 0.21648 0.12963, 0.11751 0.20699, 0.11737 0.24054, 0.11385 0.28571, 0.09277 0.34885, 0.07981 0.4127, 0.02934 0.55067, −0.02808 0.69306, −0.0469 0.75422, −0.05749 0.80562, −0.05986 0.84371, −0.05629 0.87459, −0.04921 0.90035, −0.03859 0.92121, −0.00235 0.97436, −0.00338 1.00302, 0.00461 1.00413, 0.00934 0.974, −0.00366 0.94692, −0.02113 0.92063, −0.03404 0.89499, −0.03991 0.87057, −0.03991 0.83394, −0.03286 0.79365, −0.0223 0.75824, −0.00587 0.71551, 0.00822 0.68376, 0.06916 0.56091, 0.09615 0.49741, 0.11259 0.45224, 0.12671 0.40451, 0.13498 0.3602, 0.14082 0.33968, 0.14904 0.29816, 0.15258 0.26618, 0.1608 0.24664, 0.17371 0.22222, 0.21009 0.18559, 0.4108 0.08059, 0.48005 0.0464, 0.60211 0.12088, 0.65747 0.20825, 0.67606 0.23077, 0.70775 0.28083, 0.7208 0.31071, 0.73963 0.34012, 0.77844 0.39027, 0.80047 0.41514, 0.83099 0.47009, 0.86385 0.53724, 0.89319 0.61661, 0.91432 0.70208, 0.94603 0.86837, 0.96484 0.94541, 0.97672 0.97992, 0.99448 1.00208, 0.9972 1.00479, 1.00055 1.00474, 1.0045 1.0019, 1.00464 0.99842, 1.00117 0.99512, 0.98592 0.96825, 0.98005 0.94139, 0.973 0.88034, 0.9683 0.78621, 0.96361 0.73126, 0.9542 0.67131, 0.94131 0.61905, 0.94012 0.60538, 0.93073 0.5602, 0.91667 0.50916, 0.91075 0.48072, 0.89076 0.41467, 0.86963 0.35973, 0.85197 0.32177, 0.83451 0.2906, 0.82746 0.26984, 0.81455 0.07204, 0.81559 0.0617, 0.81103 0.05861, 0.80013 0.04309, 0.79612 0.04157, 0.67276 0.01345, 0.61279 0.00367, 0.57054−0.00122, 0.55634−0.00122, 0.54941 −0.00366, 0.48122−0.00366, 0.42242−0.00244)).
2. The switched reluctance motor according to claim 1, wherein a number of rotor teeth is 12 and a number of stator poles is 18.
3. The switched reluctance motor according to claim 1, wherein a number of rotor teeth is 4 and a number of stator poles is 6.
4. The switched reluctance motor according to claim 1, wherein a number of rotor teeth is 31 and a number of stator poles is 48.
5. The switched reluctance motor according to claim 1, wherein a number of rotor teeth is 48 and a number of stator poles is 72.
6. The switched reluctance motor according to claim 1, wherein the substantially circular cylindrical envelope of the rotor has a diameter in a range of 100 mm to 150 mm.
7. The switched reluctance motor according to claim 1, wherein the rotor has a length in the range of 100 mm to 150 mm.
US18/495,678 2023-10-26 2023-10-26 Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile Active US12142973B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US18/495,678 US12142973B1 (en) 2023-10-26 2023-10-26 Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile
PCT/GB2024/052708 WO2025088317A1 (en) 2023-10-26 2024-10-23 Switched Reluctance Electrical Motors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US18/495,678 US12142973B1 (en) 2023-10-26 2023-10-26 Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile

Publications (1)

Publication Number Publication Date
US12142973B1 true US12142973B1 (en) 2024-11-12

Family

ID=93376679

Family Applications (1)

Application Number Title Priority Date Filing Date
US18/495,678 Active US12142973B1 (en) 2023-10-26 2023-10-26 Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile

Country Status (2)

Country Link
US (1) US12142973B1 (en)
WO (1) WO2025088317A1 (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130257188A1 (en) * 2012-03-30 2013-10-03 General Electric Company Flux-switching electric machine
JP2015171181A (en) * 2014-03-05 2015-09-28 株式会社ミツバ Switched reluctance motor
CN105207434A (en) * 2014-06-23 2015-12-30 罗伯特·博世有限公司 Rotor lamination for switched reluctance motors and switched reluctance motor
US20180159415A1 (en) * 2015-05-25 2018-06-07 Aditya Auto Products & Engg. (I) Pvt. Ltd. Switched reluctance machine (srm) with parallel flux path
CN208112478U (en) * 2018-04-04 2018-11-16 石镇德 A kind of switched reluctance machines reducing radial vibration and torque pulsation
US20190173335A1 (en) * 2017-12-06 2019-06-06 Rolls-Royce Plc Switched reluctance machine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4581640B2 (en) * 2004-11-17 2010-11-17 トヨタ自動車株式会社 Vehicle drive system and vehicle equipped with the same
DE102012222624A1 (en) * 2012-12-10 2014-06-12 Robert Bosch Gmbh Rotor for electrochemical combustion engine used in switched reluctance machine, has rotor tooth with nose that is protruded transverse to radial direction of rotor main portion
CN104319921A (en) * 2014-11-20 2015-01-28 北京理工大学 Switching magnetic flux motor rotor reducing torque fluctuation

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130257188A1 (en) * 2012-03-30 2013-10-03 General Electric Company Flux-switching electric machine
JP2015171181A (en) * 2014-03-05 2015-09-28 株式会社ミツバ Switched reluctance motor
CN105207434A (en) * 2014-06-23 2015-12-30 罗伯特·博世有限公司 Rotor lamination for switched reluctance motors and switched reluctance motor
US20180159415A1 (en) * 2015-05-25 2018-06-07 Aditya Auto Products & Engg. (I) Pvt. Ltd. Switched reluctance machine (srm) with parallel flux path
US20190173335A1 (en) * 2017-12-06 2019-06-06 Rolls-Royce Plc Switched reluctance machine
CN208112478U (en) * 2018-04-04 2018-11-16 石镇德 A kind of switched reluctance machines reducing radial vibration and torque pulsation

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
Shi, Machine Translation of CN208112478, Nov. 2018 (Year: 2018). *
Sudo, Machine Translation of CN105207434, Dec. 2015 (Year: 2015). *
Sudo, Machine Translation of JP2015171181, Sep. 2015 (Year: 2015). *

Also Published As

Publication number Publication date
WO2025088317A1 (en) 2025-05-01

Similar Documents

Publication Publication Date Title
JP3415406B2 (en) Magnet-embedded AC motor and its design method
JP3772115B2 (en) Brushless motor
JP5093339B2 (en) Permanent magnet rotating electric machine
JPH0614514A (en) Permanent magnet type stepping motor
JP2004304928A (en) Brushless motor
JP2006340487A (en) Brushless motor
JP6138075B2 (en) 2-phase synchronous motor
EP1261103A1 (en) Brushless dc motor
US9800123B2 (en) Method for modifying stator tooth top arc of brushless DC motor
JP2004159492A (en) Permanent magnet rotating electric machine
JP2003134772A (en) Permanent magnet dynamo-electric machine
US12142973B1 (en) Rotor for switch reluctance electrical motor with teeth having irregular cross-sectional profile
JPH10304634A (en) Permanent magnet type synchronous machine
JP7412362B2 (en) Rotating electrical machine with rotor configuration to reduce torque ripple
JP2004088855A (en) DC motor rotor and DC motor
JP4468740B2 (en) motor
JP2000166135A (en) Brushless motor
JP4234982B2 (en) Single phase induction motor
JPH05252675A (en) Generator and method for improving operating characteristics of generator
JP4172863B2 (en) 5-phase permanent magnet motor
JP2003348809A (en) Inner rotor type motor with magnet
JP3239073B2 (en) Permanent magnet field type brush motor
JP2000060092A (en) Multi-pole generator
KR101106444B1 (en) BLC motor
JP2005192263A (en) Permanent magnet motor

Legal Events

Date Code Title Description
FEPP Fee payment procedure

Free format text: ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: BIG.); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY

FEPP Fee payment procedure

Free format text: ENTITY STATUS SET TO SMALL (ORIGINAL EVENT CODE: SMAL); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY

STCF Information on status: patent grant

Free format text: PATENTED CASE